N132TS2006 Diamond DA 42
Safety record in brief:No NTSB accidents or incidents since 198225 ADs may apply17 service difficulty reports
Registration
FAA Aircraft Registry · Oct 17, 2026- Registered owner
- Utah State University
- Owner type
- Government
- City, state
- Logan, UT
- Certificate issued
- Jun 16, 2016
- Expires
- Jun 30, 2029
- Airworthiness
- Standard · Normal
- Airworthiness date
- Dec 4, 2006
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Diamond
- Model
- DA 42
- Year
- 2006
- Serial number
- 42.AC018
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 4
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A08459
Engine
- Make and model
- Thielert Tae-125-01
- Type
- Reciprocating
- Power
- 132 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2016 – nowUtah State UniversityLogan, UT · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (25)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2026-14-08 | Diamond Aircraft Industries GmbH | Jul 20, 2026 | Airframe (DA 42) |
| 2025-24-07 | Passenger/Crew Doors | Feb 12, 2026 | Airframe (DA 42) |
| 2024-06-13 | Flight Control System | May 28, 2024 | Airframe (DA 42) |
| 2022-06-08 | Flight Control System | May 9, 2022 | Airframe (DA 42)Only with: Flap bell crank P/N D60-2757-11-00, up to and including revision "f", installed. |
| 2021-22-03 | Nose/Tail Landing Gear Attach Section | Dec 21, 2021 | Airframe (DA 42) |
Show all 25 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2018-10-10 | Engine Exhaust | Jun 12, 2018 | Airframe (DA 42)Certain serial numbers: DA 42 42.004–42.427; DA 42 42.AC001–42.AC151. Only with: TAE 125-02-99 or TAE 125-02-114 engine installed and equipped with original exhaust pipe DAI P/N D60-9078-06-01 or Technify P/Ns 52-7810-H0001 02/03/04, or modified exhaust pipe DAI P/N D60-9078-06-01_01 or Technify 52-7810-H0014 01. |
| 2015-02-01 | Technify Motors GmbH (Type Certificate Previously Held by Thielert Aircraft Engines… | Feb 13, 2015 | Engine (TAE-125-01)Serial numbers per TMG SB No. TM TAE 125-0021, Revision 2, or TAE SB No. TM TAE 125-1011 P1, Revision 2. Only with: Clutch assembly P/N 02-7210-11001R11, 02-7210-11001R11-AT, 02-7210-11001R13, 05-7211-K006001, or 05-7211-K006002 with S/N listed in the referenced SBs installed. |
| 2013-24-06 | Thielert Aircraft Engines GmbH Reciprocating Engines | Dec 30, 2013 | Engine (TAE-125-01) |
| 2013-19-11 | Landing Gear | Oct 31, 2013 | Airframe (DA 42) |
| 2013-07-01 | Landing Gear | May 20, 2013 | Airframe (DA 42) |
| 2012-26-13 | Thielert Aircraft Engines GmbH Reciprocating Engines | Feb 13, 2013 | Engine (TAE-125-01) |
| 2012-17-07 | Wings | Oct 11, 2012 | Airframe (DA 42)Certain serial numbers: 42.006–42.008; 42.010; 42.012–42.014; 42.016–42.033; 42.035–42.043; 42.045; … |
| 2011-11-07 | Diamond Aircraft Industries GmbH Model DA 42 Airplanes | Jul 6, 2011 | Airframe (DA 42) |
| 2011-10-13 | Diamond Aircraft Industries GmbH Models DA 42, DA 42 NG, and DA 42 M-NG Airplanes | Jun 17, 2011 | Airframe (DA 42) |
| 2010-14-21 | Thielert Aircraft Engines GmbH Model TAE 125-01 Reciprocating Engines | Aug 17, 2010 | Engine (TAE-125-01)Only with: Blow-by oil separators P/N 02-7250-18100R1 through R4 or 02-7250-18300R1 through R5 installed. |
| 2010-11-09 | Thielert Aircraft Engines GmbH (TAE) Models TAE 125-01 and TAE 125-02-99 Reciprocating… | Jul 13, 2010 | Engine (TAE-125-01)Only with: Engines designated with P/N 05-7200-K000301 or 02-7200-1401R1. |
| 2010-06-12 | Thielert Aircraft Engines GmbH (TAE) Models TAE 125-02-99 and TAE 125-01 Reciprocating… | Apr 20, 2010 | Engine (TAE-125-01) |
| 2010-04-06 | Thielert Aircraft Engines GmbH (TAE) Model TAE 125-01 Reciprocating Engines | Mar 30, 2010 | Engine (TAE-125-01)Certain serial numbers: TAE 125-01 …–02-01-1018 |
| 2009-24-10 | Thielert Aircraft Engines GmbH (TAE) Model TAE 125-01 Reciprocating Engines | Jan 4, 2010 | Engine (TAE-125-01)Only with: Excludes engines modified to TAE Design Modification No. 2007-001. |
| 2008-23-08 | Diamond Aircraft Industries GmbH Model DA 42 Airplanes | Dec 22, 2008 | Airframe (DA 42)Serial numbers per Diamond Aircraft Industries GmbH Mandatory Service Bulletin No. MSB-42-058. Only with: Applies to airplanes with Thielert TAE125-01 engines installed, except those with engines listed in MSB-42-058 installed with wedge locking washers and bonded-in bolts. |
| 2008-16-20 | Diamond Aircraft Industries GmbH Model DA 42 Airplanes | Sep 17, 2008 | Airframe (DA 42)Only with: Aileron bellcranks P/N DA4-2717-50-00 installed. |
| 2007-23-14 | Diamond Aircraft Industries Model DA 42 Airplanes | Dec 26, 2007 | Airframe (DA 42) |
| 2007-13-16 | Diamond Aircraft Industries GmbH Model DA 42 Airplanes | Aug 10, 2007 | Airframe (DA 42)Certain serial numbers: DA 42 42.004–on |
| 2007-12-24 | Diamond Aircraft Industries Model DA 42 Airplanes | Jul 19, 2007 | Airframe (DA 42)Certain serial numbers: DA 42 42.004–42.129; DA 42 42.177; DA 42 42.AC001 |
| 2007-12-05 | Diamond Aircraft Industries GmbH Model DA 42 Airplanes | Jul 16, 2007 | Airframe (DA 42)Certain serial numbers: 42.015; 42.028; 42.036; 42.044; 42.055; 42.059; … |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (17)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Exhaust · exhaust pipe · inflt separationJul 9, 2025
AD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEATSHIELD TO BE TIGHT ON AND SPOT WELDED IN TWO PLACES TO THE EXHAUST PIPE. THE PROBLEM IS THE HEATSHIELD SPOT WELDS FAILED AND THE HEATSHIELD IS LOOSE ON THE PIPE. THE AD MAKES IT SOUND LIKE THE EXHAUST PIPE ASSY SHOULD LAST AT LEAST 1500 HOURS BUT…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Exhaust · exhaust pipe · inflt separationJul 9, 2025
AD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEATSHIELD TO BE TIGHT ON AND SPOT WELDED IN TWO PLACES TO THE EXHAUST PIPE. THE PROBLEM IS THE HEATSHIELD SPOT WELDS FAILED AND THE HEATSHIELD IS VERY LOOSE ON THE EXHAUST PIPE THE AD MAKES IT SOUND LIKE THE EXHAUST PIPE ASSY SHOULD LAST AT LEAST 1500…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Exhaust · exhaust pipe · inflt separationJul 9, 2025
AD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEATSHIELD TO BE TIGHT ON AND SPOT WELDED IN TWO PLACES TO THE EXHAUST PIPE. THE PROBLEM IS THE HEATSHIELD SPOT WELDS FAILED AND THE HEATSHIELD IS LOOSE ON THE EXHAUST PIPE AND HAS A HOLE IN THE EXHAUST PIPE CAUSED WHEN THE UPPER SPOT WELD FAILED THE AD…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Exhaust · exhaust pipe · separatedApr 15, 2025
AD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEAT SHIELD TO BE TIGHT ON THE AND WELDED TO THE EXHAUST PIPE. THE HEAT SHIELD SPOT WELDS FAILED AND VERY LOOSE ON THE EXHAUST PIPE. THE AD IS SUGGESTING THE PIPE SHOULD LAST AT LEAST 1500.0 HOURS BUT FAILED AT 68.1
From FAA Service Difficulty Reports; matched by N-number and serial number. - Exhaust · exhaust pipe · separatedFeb 25, 2025
AD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEAT SHIELD TO BE TIGHT ON AND WELDED TO THE EXHAUST PIPE. THE HEAT SHIELD SPOT WELDS FAILED AND VERY LOOSE ON THE EXHAUST PIPE THE AD IS SUGGESTING THE PIPE SHOULD LAST AT LEAST 1500 HOURS BUT FAILED AT 62.8
From FAA Service Difficulty Reports; matched by N-number and serial number. - Exhaust · exhaust pipe · brokenJan 29, 2025
EXHAUST HEAT SHIELD IS LOOSE ON THE EXHAUST PIPE AND THE WELDS HAVE FAILED. AD 2018-10-10 REQUIRES THE HEAT SHIELD TO BE TIGHT AND WELDED TO THE PIPE. THE ISSUE IS THE HEAT SHIELD IS CRIMPED ON THE PIPE AND THEN WELDED TO IT AND IT'S NOT WORKING. THIS PIPE FAILED WITH ONLY 23.5 TTSN
From FAA Service Difficulty Reports; matched by N-number and serial number. - Exhaust · exhaust pipe · separatedJan 17, 2025
AD 2018-10-10 DATED JUNE 12 2018 REQUIRES US TO INSPECT THE EXHAUST PIPES TO MAKE SURE THE HEAT SHIELD IS TIGHT ON THE EXHAUST PIPE AND THE MOUNT CLAMPS ARE NOT BROKEN EVERY 25 HOURS AND DOES NOT ALLOWED ANY ISSUES WITH THE HEATSHIELD BEING TIGHT ON THE EXHAUST PIPE AND NO CRACKS OR HOLES. AN…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Exhaust · exhaust pipe · separatedJan 17, 2025
AD 2018-10-10 DATED JUNE 12 2018 REQUIRES US TO INSPECT THE EXHAUST PIPES TO MAKE SURE THE HEAT SHIELD IS TIGHT ON THE EXHAUST PIPE AND THE MOUNT CLAMPS ARE NOT BROKEN EVERY 25 HOURS AND DOES NOT ALLOWED ANY ISSUES WITH THE HEATSHIELD BEING TIGHT ON THE EXHAUST PIPE AND NO CRACKS OR HOLES. AN…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Exhaust · exhaust pipe · separatedJan 17, 2025
AD 2018-10-10 DATED JUNE 12 2018 REQUIRES US TO INSPECT THE EXHAUST PIPES TO MAKE SURE THE HEAT SHIELD IS TIGHT ON THE EXHAUST PIPE AND THE MOUNT CLAMPS ARE NOT BROKEN EVERY 25 HOURS AND DOES NOT ALLOWED ANY ISSUES WITH THE HEATSHIELD BEING TIGHT ON THE EXHAUST PIPE AND NO CRACKS OR HOLES. AN…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Exhaust · exhaust pipe · separatedJan 17, 2025
AD 2018-10-10 DATED JUNE 12 2018 REQUIRES US TO INSPECT THE EXHAUST PIPES TO MAKE SURE THE HEAT SHIELD IS TIGHT ON THE EXHAUST PIPE AND THE MOUNT CLAMPS ARE NOT BROKEN EVERY 25 HOURS AND DOES NOT ALLOWED ANY ISSUES WITH THE HEATSHIELD BEING TIGHT ON THE EXHAUST PIPE AND NO CRACKS OR HOLES. AN…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 17 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026